N522US, cancelled Jul 21, 2017

Service difficulty reports · 42

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N522US' AND deregistration_id = 'N522US-2017-07-21'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA14036405522Battery Pack · inoperativeFOUND EMERGENCY LIGHTS, FLOOR, FROM ROW 22 TO FWD OF THE R3 DOOR INOPERATIVE. R & R BATTERY PACK IAW AMM 35-51. OPS CHECKED GOOD, OK FOR SERVICE.Jun 17, 2014 · N522US · Boeing 757251 · Emergency LightingSDR DALA14027385522Plate · corrodedL1 DOOR LOWER HINGE LOWER CAM PLATE RUSTED. REMOVED CORROSION FROM LOWER CAM PLATE AT L1 DOOR IAW ERA 476391-14MA, REV B, SECTION 1. PAINTED AND REPAIRED LOWER CAM PLATE AT L1 DOOR IAW ERA 476391-14MA, REV B, SECTION 1.Apr 30, 2014 · N522US · Boeing 757251 · Passenger/Crew DoorsSDR DALA14027005522Cam · corrodedR1 DOOR LOWER HINGE UPPER AND LOWER CAM PLATES RUSTED. REMOVED CORROSION IAW ERA 476391-14MA, REV B. CORROSION LEVEL 1. REPAIRED IAW ERA 476391-14MA, REV B, SECTION 1.Apr 29, 2014 · N522US · Boeing 757251 · Passenger/Crew DoorsSDR DALA14010625522Wire · brokenEMERGENCY LIGHT HAS A BROKEN WIRE. REPAIRED WIRING AT 20D. INSTALLED NEW LAMP. OK FOR SERVICE.Feb 18, 2014 · N522US · Boeing 757251 · Light System WiringSDR DALA14007015522Light · inoperativeDURING SERVICE CHECK, FOUND EMERGENCY LIGHT 26L BULLNOSE INOPERATIVE. SECURED 26L BULLNOSE EMERGENCY LIGHT, OPS CHECKED GOOD, OK FOR SERVICE.Jan 31, 2014 · N522US · Boeing 757251 · Emergency LightingSDR DALA13044435522Skin · scratchedFOUND A 7 INCH LONG SCRATCH IN FUSELAGE APPOXIMATELY 12 INCHES AFT OF L3 COCKPIT WINDOW LOWER AFT CORNER AND 10 INCHES BELOW LAP SEAM. BLENDED AND ACCOMPLISHED EDDY CURRENT. WITHIN LIMITS AND OK FOR SERVICE IAW SRM 53-00-01. HFEC 51-00-17 NO CRACKS.Sep 12, 2013 · N522US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA13033975522Connector · looseEMERGENCY LIGHTS ARE NOT LIGHTING IN THE AFT PART OF CABIN RESEATED CONNECTOR PLUG AT BATTERY PACK M734 IN AFT GALLEY OVERHEAD OPERATED LIGHTS ON AND OFF SEVERAL TIMES CKS NORMAL IAW AMM 33-51. OK FOR SVC.Jul 7, 2013 · N522US · Boeing 757251 · Emergency LightingSDR DALA13031445522Structure · puncturedACS REPORTED FORWARD CARGO DOOR C1, AFT LOWER CORNER EDGE PUNCTURED .75 X .25. ACFT PREPARED FOR MX FERRY FOR MAJOR REPAIRS. ACFT CURRENTLY OUT OF SERVICE.Jun 20, 2013 · N522US · Boeing 757251 · Cargo/Baggage DoorsSDR DALA13006585522Battery Pack · inoperativeDOOR 4L EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51.Feb 10, 2013 · N522US · Boeing 757251 · Emergency LightingSDR DALA12007405522Spar Cap · corrodedREAR SPAR CAP CORRODED AT RT HORIZONTAL STAB STA 318.949, COMPLIED WITH ERA 506884-14 REV. ORIG STEPS 1-14 ON PRI ERA 506884-14 REV ORIG AND REV 1.Sep 16, 2012 · N522US · Boeing 757251 · Horizontal Stabilizer, Spar/RibSDR DALA12006965522Sill · corrodedSMALL AREA OF CORROSION NR 2 CARGO DOOR LOWER SILL BS 1420. CLEANED AREA, REMOVED CORROSION PER SRM 53-60-15. AREA OUT OF LIMITS PER SRM 53-60-15. REMOVED FITTINGS FOR ACCESS. COMPLIED WITH PRI 506838-14 C/W ERA 506838-14 REV ORIG. REINSTALLED FITTINGS.Sep 11, 2012 · N522US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1238905522Connector · damagedDURING FLIGHT, EMERGENCY EXIT DOOR AND CELING LIGHTS COME ON AT DOOR 3 BOTH SIDES AND DOOR 2 RIGHT SIDE. EMERGENCY EXIT FLOOR LIGHTS COME ON IN FLIGHT FROM DOOR 3 FORWARD TO ROW 26. CYCLED EMERGENCY LIGHT SWITCH IN FLT DECK PER MC AND LIGHTS WENT OUT. FOUNDJun 23, 2012 · N522US · Boeing 757251 · Light System WiringSDR DALA1159625522Battery Pack · dischargedEXIT LIGHT ABOVE L3 DOOR INOP. REPLACED BATTERY PACK PER AMM 33-51. OPS CHECK NORMAL.Oct 24, 2011 · N522US · Boeing 757251 · Emergency LightingSDR DALA1106595522Power Supply · inoperativeDURING A LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHTS BETWEEN ROWS 22 AND 32 INOPERATIVE. MX REPLACED THE POWER SUPPLY. OPS CHECK WAS GOOD.Jan 27, 2011 · N522US · Boeing 757251 · Emergency LightingSDR DALA1102185522Tab · delaminatedLT ELEVATOR CONTROL TAB DELAMINATED APPROX 8 SQUARE INCHES. R & R RT ELEVATOR CONTROL TAB IAW AMM 27-30-03. ADJUSTMENT/TEST GOOD IAW MM 27-30-03-201 CORRECTED BY COOK 284650 STA DHN 10JAN11. REQUIRED INSP COMPLETED.Nov 24, 2010 · N522US · Boeing 757251 · Elevator, Tab StructureSDR DALA1023405522Battery Pack · inoperativeDURING A LINE CHECK, MX FOUND THE EMERGENCY EXIT LIGHT AT DOOR 2 LT INOPERATIVE. MX REPLACED THE BATTERY AND POWER SUPPLY. OPS CHECK WAS GOOD.Sep 18, 2010 · N522US · Boeing 757251 · Emergency LightingSDR DALA1023315522Gate · corrodedDURING M-CHECK FOUND CORROSION ON R1 DOOR LOWER GATE. REPAIRED IAW SRM 51-40-02, SRM 52-11-38-004.Sep 17, 2010 · N522US · Boeing 757251 · Passenger/Crew DoorsSDR DALA1022275522Bulkhead Web · damagedDURING M-CHECK FOUND DAMAGE TO BULKHEAD WEB IN NR 2 PYLON MID SPAR BULKHEAD FITTING FWD FACE. REPAIRED IAW ERA 484910-14.Sep 12, 2010 · N522US · Boeing 757251 · Nacelle/Pylon, Bulkhead/FirewallSDR DALA1022265522Skin · dentedDURING M-CHECK FOUND DENT AND SCRATCH ON FUSELAGE SKIN AT BS 620 S16L. REPAIRED IAW ERA 484243-14.Sep 10, 2010 · N522US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1020805522Floor Support · corrodedCORROSION ON CABIN FLOOR SUPPORT BEAM FROM STA 345-377 BL'0'. REMOVED CORROSION FROM FLOOR SUPPORT BEAM BL'0' BTW STA 345-377 IAW SRM 51-10-02. ORIGINAL MAT. .063" MAT LOSS .016 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51 FIG 101. REMOVED FLOOR SUPPORT BEAM IAAug 31, 2010 · N522US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1020795522Floor Support · corrodedCORROSION ON CABIN FLOOR SUPPORT BEAM STA 405 RBL24 STA BFM. REMOVED CORROSION DIM. L=2.5" W=.800" D=.071" FOUND TO BE OUT LIMITS IAW SRM 53-00-51. REMOVED FLOOR SUPPORT BEAM STA 365-440 RBL24 IAW SRM 51-40-02, REMOVED FLOOR BOX BEAM IAW SRM 51-40-02 LOCATEDAug 31, 2010 · N522US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1020785522Floorbeam · corrodedCORROSION ON CABIN FLOORBEAM STA 377,BL'0' TO LBL18 AND AT RBL13. RII: Y BLENDED AREA ORG .125 L=3" X W=1.2" X D=.035 REMAINING .090 OUT OF LIMITS IAW SRM 53-00-51, FIG 101 SHEET 1,2,3 DETAIL II,III. REMOVED SPLICES AT STA 377 RBL32 & LBL34 IAW SRM 51-40-02. RAug 31, 2010 · N522US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA1020775522Wedge · damagedRT WING, SLAT NR7, T/E WEDGE, APPROX 36" FROM OTBD EDGE IS DAMAGED. REMOVED DAMAGED SKIN AND CORE AND BONDED NEW CORE INTERNAL DOUBLER FILLER AND EXTERNAL DOUBLER IAW SRM 51-70-10 REPAIR NR 4, FIG 202. PAINTED AREA IAW MM 51-21-10. RII COMPLETED BY SAN 489916Aug 28, 2010 · N522US · Boeing 757251 · Leading Edge DevicesSDR DALA1020765522Skin · damagedRT WING SLAT NR 7 T/E WEDGE, APPROX 36" FROM INBD EDGE IS DAMAGED. REMOVED DAMAGED SKIN AND CORE AND BONDED NEW CORE, INTERNAL DOUBLER FILLER, AND EXTERNAL DOUBLER IAW SRM 51-70-10, REPAIR NR4, FIG 200. COMPLETED BY SAN 489916, STAMP 91.Aug 28, 2010 · N522US · Boeing 757251 · Leading Edge DevicesSDR DALA1020755522Wedge · damagedRT WING SLAT NR 8 T/E WEDGE APPROX 36" FROM INBD EDGE IS DAMAGED. RII: Y. REMOVED INNER SKIN, CORE AND EXTERNAL SKIN. FABRICATED NEW SKIN AND CORE AND BONDED IAW SRM 51-70-10 REPAIR NR4, FIG 202. PAINTED IAW MM 51-21 -10. RII COMPLETED BY SAN 489916 STAMP 91.Aug 28, 2010 · N522US · Boeing 757251 · Leading Edge DevicesSDR DALA1020745522Floorbeam · corrodedCORROSION ON CABIN FLOORBEAM UPPER CHORD AT STA 365 FROM RBL 63-BL'0'. BLENDED AREA DIM. L=5' W=2" D=.060" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, REMOVED OLD REPAIR IAW SRM 51-40-02. FAB, LOCATED, & DRILLED T-CHORD BEAM IAW SRM 51-40-05 & 53-00-51, INSTAAug 28, 2010 · N522US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA1020515522Floorbeam · corrodedDURING "M" CHECK FOUND CORROSION ON FLOORBEAM AT BS 1640. REPAIRED IAW SRM 51-40-02 & SRM 53-00-01, FIG 201.Aug 26, 2010 · N522US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA1020505522Web · corrodedDURING "M" CHECK FOUND CORROSION ON FLOOR WEB AT BS 1718 BL 0 TO RBL 31. REPAIRED IAW SRM 51-40-02, SRM 53-60-51 REPAIR NR 2.Aug 26, 2010 · N522US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1020495522Floorbeam · corrodedDURING M-CHECK FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 345 BL 0 TO LBL 18. REPAIRED IAW SRM 53-00-51 REPAIR NR 5.Aug 26, 2010 · N522US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA1020325522Web · corrodedDURING M-CHECK, FOUND CORROSION ON WEB AT STRINGER 27R BETWEEN BS 1360 & BS 1380. REPAIRED IAW SRM 51-40-02.Aug 24, 2010 · N522US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1019535522Skin · dentedDURING M-CHECK FOUND DENT IN LOWER FUSELAGE SKIN BETWEEN BS 660 & BS 680 STRINGER 23L & STRINGER 24L. REPAIRED IAW SRM 53-00-01 FIG 201, SRM 51-42-11.Aug 17, 2010 · N522US · Boeing 757251 · Fuselage Main, Plate/SkinSDR 0103795522Slide · rupturedDURING SLIDE SHOP TEST, INFLATABLE SUB ASSEMBLY SEAM RUPTURED AT NORMAL OPERATING PRESSURE. NEW INFLATABLE SUB ASSEMBLY WAS INSTALLED.Oct 22, 2001 · N522US · Boeing 757251 · Escape SlideSDR 0101295522Annunciator · smokeUPON ARRIVAL TO GATE, FLIGHT CREW NOTICED SMOKE COMING FROM THE LANDING GEAR CONTROL HANDLE OPENING. FIRE EQUIPMENT WAS CALLED OUT. AFTER SHUTDOWN OF ENGINE, APU, AND UTILITY BUSSES, THE SMOKE STOPPED. MAINTENANCE REPLACED THE LEFT LANDING GEAR DOWN ANNUNCIApr 4, 2001 · N522US · Boeing 757251 · Landing Gear Position and WarningSDR 9719055522Fseu · malfunctionedDURING FINAL APPROACH, L/E FLAP ASSYM ANNUNCIATED. FLIGHT CREW DECLARED AN EMERGENCY AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED NR 1 FSEU.Oct 13, 1997 · N522US · Boeing 757251 · Leading Edge Slat Control SystemSDR 9719045522Fseu · malfunctionedDURING FINAL APPROACH, L/E FLAP ASSYM AND LEADING EDGE CAUTION LIGHT ILLUMINATED. GO-AROUND ACCOMPLISHED FOLLOWED BY UNEVENTFUL LANDING. MAINTENANCE REPLACED NR 2 FSEU.Oct 12, 1997 · N522US · Boeing 757251 · Leading Edge Slat Control SystemSDR 9716945522Fitting · corrodedDURING TRANSITION CHECK, FOUND CORROSION ON THE THIRD FROM FORWARD FITTING AT THE FORWARD CARGO DOOR THRESHOLD AT FS 580. REPLACED FITTING PER SRM 51-10-00.Sep 8, 1997 · N522US · Boeing 757251 · Fuselage Miscellaneous StructureSDR 9716935522Fitting · corrodedDURING TRANSITION CHECK, FOUND CORROSION ON THE SECOND FROM AFT FITTING AT THE FORWARD CARGO DOOR THRESHOLD FS 610. REPLACED FITTING PER SRM 51-10-00.Sep 8, 1997 · N522US · Boeing 757251 · Fuselage Miscellaneous StructureSDR 9716925522Fitting · corrodedDURING TRANSITION CHECK, FOUND CORROSION ON THE SECOND FROM FORWARD FITTING AT THE FORWARD CARGO DOOR THRESHOLD FS 570. REPLACED FITTING PER SRM 51-10-00.Sep 8, 1997 · N522US · Boeing 757251 · Fuselage Miscellaneous StructureSDR 9717315522Floorbeam · corrodedDURING TRANSITION CHECK, FOUND CORROSION ON TOP OF FLOORBEAM AT SEVERAL LOCATIONS FROM LBL 54 TO RBL 24, FS 1680. REPAIRED PER EA 55-151991.Sep 4, 1997 · N522US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9610005522Floor Beam · corrodedDURING P-CHECK, FOUND CORROSION ON THE BS 1681 FLOOR BEAM UPPER CHORD AT LBL 32. REPAIRED CHORD (P/N 146N5091) PER EA 55-102159.Apr 26, 1996 · N522US · Boeing 757251 · Fuselage Main, Floor BeamSDR 9510465522Outflow Act · malfunctionedDURING CLIMB, BOTH AUTO PRESSURE CONTROLLERS WERE INOPERATIVE WITH CABIN AUTO INOPERATIVE STATUS MESSAGE. AIRCRAFT RETURNED TO MSP. REPLACED OUTFLOW VALVE ACTUATOR. SYSTEM CHECK WAS NORMAL.Jul 8, 1995 · N522US · Boeing 757251 · Pressure Regulator/Outflow ValveSDR 9508755522Bleed Valve · failedDURING CLIMB, THE NR 2 COMPRESSOR STALLED TWICE. TWO LOUD BANGS AND A BRIGHT FLASH WERE OBSERVED. NO ABNORMAL ENGINE INDICATIONS WERE OBSERVED. AIRCRAFT WAS RETURNED TO MEM WHERE TROUBLESHOOTING FOUND THE 2.5 BLEED VALVE SEIZED. THE ENGINE WAS REPLACED.May 28, 1995 · N522US · Boeing 757251 · Compressor Bleed Valve
Back to N522US, cancelled Jul 21, 2017